Producing semi-crystalline pulverulent polycarbonate and use thereof in additive manufacturing

ABSTRACT

Ways of preparing a partially crystalline polycarbonate powder are provided that include dissolving an amorphous polycarbonate in a polar aprotic solvent to form a first solution of solubilized polycarbonate at a first temperature. The first solution is then cooled to a second temperature, the second temperature being lower than the first temperature, where a portion of the solubilized polycarbonate precipitates from the first solution to form a second solution including the partially crystalline polycarbonate powder. Certain partially crystalline polycarbonate powders resulting from such methods are particularly useful in additive manufacturing processes, including powder bed fusion processes.

FIELD

The present technology relates to precipitating a pulverulentpolycarbonate in a solvent, allowing the pulverulent polycarbonate toform crystallites, and employing the precipitated pulverulentpolycarbonate in a powder-based additive manufacturing process.

BACKGROUND OF THE INVENTION

This section provides background information related to the presentdisclosure which is not necessarily prior art.

Various additive manufacturing processes, also known asthree-dimensional (3D) printing processes, can be used to formthree-dimensional objects by fusing certain materials at particularlocations and/or in layers. Material can be joined or solidified undercomputer control, for example working from a computer-aided design (CAD)model, to create a three-dimensional object, with material being addedtogether, such as liquid molecules or powder grains being fusedtogether, typically layer-by-layer. Various types of additivemanufacturing include binder jetting, directed energy deposition,material extrusion, material jetting, powder bed fusion, sheetlamination, and vat photopolymerization.

Certain additive manufacturing methods can be conducted usingthermoplastic polymers (e.g., polycarbonate), which include materialextrusion, fused deposition modeling, and powder bed fusion. Powder bedfusion, in general, involves selective fusing of materials in a powderbed. The method can fuse parts of a layer of powder material, moveupward in a working area, add another layer of powder material, andrepeat the process until an object is built up therefrom. The powder bedfusion process can use unfused media to support overhangs and thin wallsin the object being produced, which can reduce the need for temporaryauxiliary supports in forming the object. In selective heat sintering, athermal printhead can apply heat to layers of powdered thermoplastic;when a layer is finished, the powder bed moves down, and an automatedroller adds a new layer of material which is sintered to form the nextcross-section of the object. Selective laser sintering is another powderbed fusion process that can use one or more lasers to fuse powderedthermoplastic polymers into the desired three-dimensional object.

Materials for powder bed fusion processes preferably have a uniformshape, size, and composition. The preparation of such powders fromthermoplastic polymers on an economical and large scale is notstraightforward. What is more, it can be difficult to use amorphouspolycarbonates, particularly in powder bed fusing processes such asselective laser sintering, because such polycarbonates may not exhibit asharp melting point. This property can result in dissipation of theapplied thermal energy source (e.g., a laser beam) into the regionssurrounding where the energy source contacts or strikes the powder bed.This undesired dissipation of thermal energy can result in unstableprocessing as well as poor feature resolution in the intendedthree-dimensional object being produced.

Certain preparations of polycarbonate powders for powder bed fusion areknown. For example, U.S. Pub. No. 2017/9567443 B2, Japanese Pat. No.2017/095650 A, and U.S. Pub. No. 2018/0244863 A1 each discuss methodsthat include dissolving polycarbonate in a suitable organic solvent,addition of a dispersing polymer to promote and sustain emulsionformation, and addition of a solvent that is miscible with the organicsolvent but that is not a solvent for the polycarbonate, resulting inemulsion formation and subsequent precipitation of polycarbonate powder.In addition, WO 2018/071578 A1 and U.S. Pub. No. 2018/0178413 A1describe the use of solvents to induce crystalline domain formation inpre-formed powder particles produced from grinding methods.

Such methods of preparing crystalline polycarbonate powders for use inpowder bed fusion processes still present several technical issues. Inparticular, prior methods of processing polycarbonate powder into a formsuitable for use in certain methods, such as selective laser sintering(SLS), multi jet fusion (MJF), high speed sintering (HSS), andelectrophotographic 3D-printing applications, can require the use ofmixed solvents and dispersants. There is accordingly a need to provide asingle solvent method, facilitating solvent recovery and reuse, that canform polycarbonate powder having optimal crystallinity and optimalparticle size distribution from amorphous polymer, where the crystallinepolycarbonate powder results in improved powder bed fusion performance.

SUMMARY OF THE INVENTION

The present technology includes processes, compositions, and articles ofmanufacture that relate to preparation of a partially crystallinepolycarbonate powder and use thereof in additive manufacturingprocesses, including powder bed fusion processes.

Methods of preparing a partially crystalline polycarbonate powder areprovided that include dissolving an amorphous polycarbonate in a polaraprotic solvent to form a first solution of solubilized polycarbonate ata first temperature. The first solution is then cooled to a secondtemperature, where the second temperature is lower than the firsttemperature. A portion of the solubilized polycarbonate precipitatesfrom the first solution to form a second solution including thepartially crystalline polycarbonate powder. Powder compositions for usein powder bed fusion processes are provided that include a partiallycrystalline polycarbonate powder prepared by such methods. Objects canbe prepared by using such partially crystalline polycarbonate powders ina powder bed fusion process to form the object.

The disclosed exemplary apparatuses, systems, and methods provide powderpolycarbonate having a suitable operating window for use in SLS, MJF,HSS, and electrophotography 3D-printing applications. An embodiment ofthe disclosure may provide a precipitated pulverulent polycarbonateformed through precipitating the polycarbonate in a solvent, allowingthe polymer to form crystallites, and then employing the precipitatedpulverulent polycarbonate in a powder-based 3D-printing process.

Further areas of applicability will become apparent from the descriptionprovided herein. The description and specific examples in this summaryare intended for purposes of illustration only and are not intended tolimit the scope of the present disclosure.

BRIEF DESCRIPTION OF THE DRAWINGS

The drawings described herein are for illustrative purposes only ofselected embodiments and not all possible implementations, and are notintended to limit the scope of the present disclosure.

FIG. 1 : Low vacuum secondary electron detector (LVSED) scanningelectron micrograph (SEM) of pulverulent polycarbonate as produced byExample 1, magnification 50×.

FIG. 2 : Low vacuum secondary electron detector (LVSED) scanningelectron micrograph (SEM) of pulverulent polycarbonate as produced byExample 1, magnification 500×.

FIG. 3 : Differential scanning calorimetry (DSC) of pulverulentpolycarbonate as produced by Example 1.

FIG. 4 : Selective laser sintering (SLS) process to produce samplecoupon from pulverulent polycarbonate as described in Example 1.

FIG. 5 : Selective laser sintering (SLS) process to produce sampletensile bars from pulverulent polycarbonate as described in Example 3.

FIG. 6 : Selective laser sintered (SLS) 1 in. cube printed frompulverulent polycarbonate as described in Example 3. Sides were polishedto remove exterior powder coating and expose the interior of the part.

DETAILED DESCRIPTION

The following description of technology is merely exemplary in nature ofthe subject matter, manufacture and use of one or more inventions, andis not intended to limit the scope, application, or uses of any specificinvention claimed in this application or in such other applications asmay be filed claiming priority to this application, or patents issuingtherefrom. Regarding methods disclosed, the order of the steps presentedis exemplary in nature, and thus, the order of the steps can bedifferent in various embodiments. “A” and “an” as used herein indicate“at least one” of the item is present; a plurality of such items may bepresent, when possible. Except where otherwise expressly indicated, allnumerical quantities in this description are to be understood asmodified by the word “about” and all geometric and spatial descriptorsare to be understood as modified by the word “substantially” indescribing the broadest scope of the technology. “About” when applied tonumerical values indicates that the calculation or the measurementallows some slight imprecision in the value (with some approach toexactness in the value; approximately or reasonably close to the value;nearly). If, for some reason, the imprecision provided by “about” and/or“substantially” is not otherwise understood in the art with thisordinary meaning, then “about” and/or “substantially” as used hereinindicates at least variations that may arise from ordinary methods ofmeasuring or using such parameters.

All documents, including patents, patent applications, and scientificliterature cited in this detailed description are incorporated herein byreference, unless otherwise expressly indicated. Where any conflict orambiguity may exist between a document incorporated by reference andthis detailed description, the present detailed description controls.

Although the open-ended term “comprising,” as a synonym ofnon-restrictive terms such as including, containing, or having, is usedherein to describe and claim embodiments of the present technology,embodiments may alternatively be described using more limiting termssuch as “consisting of” or “consisting essentially of.” Thus, for anygiven embodiment reciting materials, components, or process steps, thepresent technology also specifically includes embodiments consisting of,or consisting essentially of, such materials, components, or processsteps excluding additional materials, components or processes (forconsisting of) and excluding additional materials, components orprocesses affecting the significant properties of the embodiment (forconsisting essentially of), even though such additional materials,components or processes are not explicitly recited in this application.For example, recitation of a composition or process reciting elements A,B and C specifically envisions embodiments consisting of, and consistingessentially of, A, B and C, excluding an element D that may be recitedin the art, even though element D is not explicitly described as beingexcluded herein.

As referred to herein, disclosures of ranges are, unless specifiedotherwise, inclusive of endpoints and include all distinct values andfurther divided ranges within the entire range. Thus, for example, arange of “from A to B” or “from about A to about B” is inclusive of Aand of B. Disclosure of values and ranges of values for specificparameters (such as amounts, weight percentages, etc.) are not exclusiveof other values and ranges of values useful herein. It is envisionedthat two or more specific exemplified values for a given parameter maydefine endpoints for a range of values that may be claimed for theparameter. For example, if Parameter X is exemplified herein to havevalue A and also exemplified to have value Z, it is envisioned thatParameter X may have a range of values from about A to about Z.Similarly, it is envisioned that disclosure of two or more ranges ofvalues for a parameter (whether such ranges are nested, overlapping ordistinct) subsume all possible combination of ranges for the value thatmight be claimed using endpoints of the disclosed ranges. For example,if Parameter X is exemplified herein to have values in the range of1-10, or 2-9, or 3-8, it is also envisioned that Parameter X may haveother ranges of values including 1-9, 1-8, 1-3, 1-2, 2-10, 2-8, 2-3,3-10, 3-9, and so on.

When an element or layer is referred to as being “on,” “engaged to,”“connected to,” or “coupled to” another element or layer, it may bedirectly on, engaged, connected or coupled to the other element orlayer, or intervening elements or layers may be present. In contrast,when an element is referred to as being “directly on,” “directly engagedto,” “directly connected to” or “directly coupled to” another element orlayer, there may be no intervening elements or layers present. Otherwords used to describe the relationship between elements should beinterpreted in a like fashion (e.g., “between” versus “directlybetween,” “adjacent” versus “directly adjacent,” etc.). As used herein,the term “and/or” includes any and all combinations of one or more ofthe associated listed items.

Although the terms first, second, third, etc. may be used herein todescribe various elements, components, regions, layers and/or sections,these elements, components, regions, layers and/or sections should notbe limited by these terms. These terms may be only used to distinguishone element, component, region, layer or section from another region,layer or section. Terms such as “first,” “second,” and other numericalterms when used herein do not imply a sequence or order unless clearlyindicated by the context. Thus, a first element, component, region,layer or section discussed below could be termed a second element,component, region, layer or section without departing from the teachingsof the example embodiments.

Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,”“lower,” “above,” “upper,” and the like, may be used herein for ease ofdescription to describe one element or feature's relationship to anotherelement(s) or feature(s) as illustrated in the figures. Spatiallyrelative terms may be intended to encompass different orientations ofthe device in use or operation in addition to the orientation depictedin the figures. For example, if the device in the figures is turnedover, elements described as “below” or “beneath” other elements orfeatures would then be oriented “above” the other elements or features.Thus, the example term “below” can encompass both an orientation ofabove and below. The device may be otherwise oriented (rotated 90degrees or at other orientations) and the spatially relative descriptorsused herein interpreted accordingly.

The present technology provides ways to make and use partiallycrystalline polycarbonate powder, including partially crystallinepolycarbonate powder having suitable characteristics for use inselective laser sintering (SLS), multi jet fusion (MJF), high speedsintering (HSS), and electrophotographic 3D-printing. Embodimentsprovide a precipitated pulverulent polycarbonate formed throughprecipitating the polycarbonate in a solvent, allowing the polymer toform crystallites, and then employing the precipitated pulverulentpolycarbonate in a powder-based 3D-printing process. The presentpartially crystalline polycarbonate powder exhibits optimizedcharacteristics for powder bed fusion processes, including optimizedparticle size, shape, distribution, and crystallinity, while at the sametime using a dispersant-free single-solvent process in manufacturethereof.

Methods of preparing a partially crystalline polycarbonate powder caninclude dissolving an amorphous polycarbonate in dimethyl sulfoxide(DMSO) solvent to form a solution at elevated temperature; cooling thesolution to room temperature to form a pulverulent, partiallycrystalline polycarbonate precipitate having a D90 particle size of lessthan 150 μm; an average particle diameter of less than or equal to 100μm, or an average particle diameter of between 0 to 100 μm; and at least20% crystallinity, or at least 25% crystallinity, or 25 to 35%crystallinity. Prior methods of processing polycarbonate powder into aform suitable for use in an additive manufacturing process, such asselective laser sintering (SLS), multi jet fusion (MJF), high speedsintering (HSS), and electrophotographic 3D-printing applications, thatrequire the use of mixed solvents and dispersants; whereas, theprocesses described herein can employ a single solvent method,facilitating solvent recovery and reuse. The methods also yield aproduct where the particles can exhibit a certain size (about 30micrometers to about 40 micrometers in average diameter), lowdispersity, spheroidal shape, and crystalline character suitable for theabove-mentioned printing processes in comparison to the results ofaforementioned processes.

In certain embodiments, methods of preparing a partially crystallinepolycarbonate powder are provided. Such methods can include dissolvingan amorphous polycarbonate in a polar aprotic solvent to form a firstsolution of solubilized polycarbonate at a first temperature. The firstsolution is then cooled to a second temperature, the second temperaturebeing lower than the first temperature, where a portion of thesolubilized polycarbonate precipitates from the first solution to form asecond solution including the partially crystalline polycarbonatepowder. The precipitated partially crystalline polycarbonate powder canbe separated from a remainder of the second solution. The separatedpartially crystalline polycarbonate powder can also be dried. It ispossible to repeat the dissolving step using the remainder of the secondsolution as the polar aprotic solvent, and further repeat the coolingstep to form the second solution including another partially crystallinepolycarbonate powder. In certain embodiments, the polar aprotic solventcan include dimethyl sulfoxide. In other embodiments, the polar aproticsolvent can consists essentially of dimethyl sulfoxide. And in stillfurther embodiments, the polar aprotic solvent can consist of dimethylsulfoxide.

Various temperatures can be employed in methods of preparing thepartially crystalline polycarbonate powder. The dissolving step caninclude heating the amorphous polycarbonate in the polar aprotic solventto form the first solution of solubilized polycarbonate at the firsttemperature, where the first temperature is greater than roomtemperature. The cooling step can include cooling the first solution tothe second temperature, where the second temperature is roomtemperature. In certain embodiments, the first solution can besupersaturated with amorphous polycarbonate at the first temperature.For example, the first solution can be supersaturated with amorphouspolycarbonate at the first temperature in comparison to the solubilitylimit of amorphous polycarbonate in the first solution at the secondtemperature.

Various embodiments of the partially crystalline polycarbonate powderprepared according to the present methods can exhibit the followingphysical characteristics. The partially crystalline polycarbonate powdercan have a D90 particle size of less than about 150 micrometers; i.e.,90 vol % of the particles in the total distribution of the partiallycrystalline polycarbonate powder have a particle diameter of 150micrometers or smaller. In certain embodiments, the partiallycrystalline polycarbonate powder can have an average particle diameterof less than about 100 micrometers. The partially crystallinepolycarbonate powder can also have an average particle diameter fromabout 1 micrometer to about 100 micrometers. Particular embodimentsinclude where the partially crystalline polycarbonate powder has anaverage particle diameter from about 30 micrometers to about 40micrometers. The partially crystalline polycarbonate powder can be inthe form of spheroidal particles. Various crystallinity values arepossible, where the partially crystalline polycarbonate powder can haveat least about 20% crystallinity, at least about 25% crystallinity, andin certain embodiments the partially crystalline polycarbonate powdercan have a crystallinity between about 25% and about 35%.

In certain embodiments, powder compositions for use in a powder bedfusion process are provided, where such powder compositions include apartially crystalline polycarbonate powder prepared according to themethods provided herein. For example, a powder composition for use in apowder bed fusion process can include a partially crystallinepolycarbonate powder having a D90 particle size of less than about 150micrometers, an average particle diameter from about 30 micrometers toabout 40 micrometers, and a crystallinity between about 25% and about35%. Such powder compositions can include mixtures of partiallycrystalline polycarbonate powders having different physicalcharacteristics as well as additives and other components as describedherein.

In certain embodiments, methods of preparing an object are provided.Such methods can include preparing a partially crystalline polycarbonatepowder by a method that includes dissolving an amorphous polycarbonatein a polar aprotic solvent to form a first solution of solubilizedpolycarbonate at a first temperature. The first solution can then becooled to a second temperature, the second temperature being lower thanthe first temperature, wherein a portion of the solubilizedpolycarbonate precipitates from the first solution to form a secondsolution including the partially crystalline polycarbonate powder. Thepartially crystalline polycarbonate powder is then used in a powder bedfusion process to form the object. Certain methods of preparing anobject include providing a partially crystalline polycarbonate powderhaving a D90 particle size of less than about 150 micrometers, anaverage particle diameter from about 30 micrometers to about 40micrometers, and a crystallinity between about 25% and about 35%. Thepartially crystalline polycarbonate powder is then used in a powder bedfusion process to form the object.

In certain embodiments, one or more objects prepared by an additivemanufacturing process are provided. Such methods can include providing apartially crystalline polycarbonate powder prepared according to one ormore of the methods described herein. The partially crystallinepolycarbonate powder is then used in a powder bed fusion process to formthe one or more objects.

In certain embodiments, the present technology includes methods ofconverting an amorphous polycarbonate to a partially crystallinepolycarbonate powder. Such methods can include dissolving the amorphouspolycarbonate in a polar aprotic solvent such as dimethyl sulfoxide(DMSO) to form a solution at an elevated temperature above roomtemperature, subsequently cooling the solution to room temperature toform a partially crystalline polycarbonate precipitate, and recoveringthe partially crystalline polycarbonate precipitate as a substantiallyuniform polycarbonate powder from the solvent. The resulting partiallycrystalline polycarbonate powder can have good crystallinity, particlesize distribution, and flowability. In particular, the partiallycrystalline polycarbonate powder can include: a D90 particle size ofless than 150 μm; an average particle diameter of less than or equal to100 μm or an average particle diameter of between 0 to 100 μm; and atleast 20% crystallinity, at least 25% crystallinity, or 25 to 35%crystallinity. As the majority of the particles of the partiallycrystalline polycarbonate powder can have a size of less than 150micrometers (μm), the partially crystalline polycarbonate powder cantherefore be effectively used in powder bed fusion processes, e.g.,selective laser sintering processes, to produce layers having athickness of 100 μm to 150 μm.

In certain embodiments, the present technology includes methods forpowder bed fusing a powder composition including the partiallycrystalline polycarbonate powder to form a three-dimensional object. Dueto the good flowability of the partially crystalline polycarbonatepowder, a smooth and dense powder bed can be formed allowing for optimumprecision and density of the sintered object. The partially crystallinenature of the polycarbonate material further allows for ease ofprocessing, where the use of crystalline polycarbonate permits the useof reduced melting energy versus the melting of corresponding amorphouspolymeric materials.

The terms “amorphous” and “crystalline” as used herein refer their usualmeanings in the polymer art, with respect to alignment of polymermolecular chains. For example, in an amorphous polymer (e.g.,polycarbonate) the molecules can be oriented randomly and can beintertwined, much like cooked spaghetti noodles, and the polymer canhave a glasslike, transparent appearance. In crystalline polymers, thepolymer molecules can be aligned together in ordered regions, much likeuncooked spaghetti noodles. In the polymer art, some types ofcrystalline polymers are sometimes referred to as “semi-crystallinepolymers.” The term “crystalline” as used herein refers to bothcrystalline and semi-crystalline polymers. The term “partiallycrystalline polycarbonate” as used herein means a portion of thepolycarbonate polymer is in crystalline form. The term “percentcrystallinity” or “% crystallinity” as used herein, refers to theportion of the amorphous polymer that has been converted to thepartially crystalline form. The percentage is based upon the totalweight of the partially crystalline polymer.

The particle size of the partially crystalline polymer can affect itsuse in additive manufacturing processes. As used herein, D50 (as knownas “average particle diameter”) refers to the particle diameter of thepowder where 50 vol. % of the particles in the total distribution of thereferenced sample have the noted particle diameter or smaller.Similarly, D10 refers to the particle diameter of the powder where 10vol. % of the particles in the total distribution of the referencedsample have the noted particle diameter or smaller; D90 refers to theparticle diameter of the powder where 90 vol. % of the particles in thetotal distribution of the referenced sample have the noted particlediameter or smaller; and D95 refers to the particle diameter of thepowder where 95 vol. % of the particles in the total distribution of thereferenced sample have the noted particle diameter or smaller. Particlesizes can be measured by any suitable methods known in the art tomeasure particle size by diameter. In some embodiments, the particlesize is determined by laser diffraction as is known in the art. Forexample, particle size can be determined using a laser diffractometersuch as the Microtrac 53500. The partially crystalline polycarbonatepowder provided herein can have a D90 particle size of less than 150 μm.

The term “high shear mixing conditions” refers to methods of agitatingthe components in a mixture (e.g., liquid mixture) under conditions inwhich high shear forces are generated. As is known in the art, a highshear mixer creates patterns of flow and turbulence, generally using animpeller that rotates inside a stator. Once the impeller has drawnmixture in, it subjects the mixture sudden changes of direction andacceleration, often approaching 90 degrees, such that the mixturecontacts the wall of the stator with centrifugal force, or is forcedthrough the holes in the stator at great pressure and speed, in a finaldisintegrating change of direction and acceleration. In certainembodiments of high shear mixing conditions, the high shear mixingcomprises mixing at speeds of 2,000 rotations per minute (rpm) to 20,000rpm, specifically, 3,000 rpm to 15,000 rpm, more specifically 4,000 rpmto 10,000 rpm. High shear mixing can be achieved with any commerciallyavailable high shear mixers. For example, a high shear mixer such as aSilverson L5M homogenizer can be used.

The term “powder bed fusing” or “powder bed fusion” is used herein tomean processes wherein the polycarbonate is selectively sintered ormelted and fused, layer-by-layer to provide a 3-D object. Sintering canresult in objects having a density of less than about 90% of the densityof the solid powder composition, whereas melting can provide objectshaving a density of 90%-100% of the solid powder composition. Use ofcrystalline polycarbonate as provided herein can facilitate melting suchthat resulting densities can approach densities achieved by injectionmolding methods.

Powder bed fusing or powder bed fusion further includes all lasersintering and all selective laser sintering processes as well as otherpowder bed fusing technologies as defined by ASTM F2792-12a. Forexample, sintering of the powder composition can be accomplished viaapplication of electromagnetic radiation other than that produced by alaser, with the selectivity of the sintering achieved, for example,through selective application of inhibitors, absorbers, susceptors, orthe electromagnetic radiation (e.g., through use of masks or directedlaser beams). Any other suitable source of electromagnetic radiation canbe used, including, for example, infrared radiation sources, microwavegenerators, lasers, radiative heaters, lamps, or a combination thereof.In certain embodiments, selective mask sintering (“SMS”) techniques canbe used to produce three-dimensional objects. For further discussion ofSMS processes, see for example U.S. Pat. No. 6,531,086, which describesan SMS machine in which a shielding mask is used to selectively blockinfrared radiation, resulting in the selective irradiation of a portionof a powder layer. If using an SMS process to produce objects frompowder compositions of the present technology, it can be desirable toinclude one or more materials in the powder composition that enhance theinfrared absorption properties of the powder composition. For example,the powder composition can include one or more heat absorbers ordark-colored materials (e.g., carbon black, carbon nanotubes, or carbonfibers).

Also included herein are all three-dimensional objects made by powderbed fusing compositions including the partially crystallinepolycarbonate powder described herein. After a layer-by-layermanufacture of an object, the object can exhibit excellent resolution,durability, and strength. Such objects can include various articles ofmanufacture that have a wide variety of uses, including uses asprototypes, as end products, as well as molds for end products.

In particular, powder bed fused (e.g., laser sintered) objects can beproduced from compositions including the partially crystallinepolycarbonate powder using any suitable powder bed fusing processesincluding laser sintering processes. These objects can include aplurality of overlying and adherent sintered layers that include apolymeric matrix which, in some embodiments, can have reinforcementparticles dispersed throughout the polymeric matrix. Laser sinteringprocesses are known, and are based on the selective sintering of polymerparticles, where layers of polymer particles are briefly exposed tolaser light and the polymer particles exposed to the laser light arethus bonded to one another. Successive sintering of layers of polymerparticles produces three-dimensional objects. Details concerning theselective laser sintering process are found, by way of example, in thespecifications of U.S. Pat. No. 6,136,948 and WO 96/06881. However, thepartially crystalline polycarbonate powder described herein can also beused in other rapid prototyping or rapid manufacturing processing of theprior art, in particular in those described above. For example, thepartially crystalline polycarbonate powder can in particular be used forproducing moldings from powders via the SLS (selective laser sintering)process, as described in U.S. Pat. No. 6,136,948 or WO 96/06881, via theSIB process (selective inhibition of bonding of powder), as described inWO 01/38061, via 3D printing, as described in EP 0 431 924, or via amicrowave process, as described in DE 103 11 438.

In certain embodiments, the present technology includes forming aplurality of layers in a preset pattern by an additive manufacturingprocess. “Plurality” as used in the context of additive manufacturingcan include 5 or more layers, or 20 or more layers. The maximum numberof layers can vary greatly, determined, for example, by considerationssuch as the size of the object being manufactured, the technique used,the capacities and capabilities of the equipment used, and the level ofdetail desired in the final object. For example, 5 to 100,000 layers canbe formed, or 20 to 50,000 layers can be formed, or 50 to 50,000 layerscan be formed.

As used herein, “layer” is a term of convenience that includes anyshape, regular or irregular, having at least a predetermined thickness.In certain embodiments, the size and configuration two dimensions arepredetermined, and in certain embodiments, the size and shape of allthree-dimensions of the layer are predetermined. The thickness of eachlayer can vary widely depending on the additive manufacturing method. Incertain embodiments the thickness of each layer as formed can differfrom a previous or subsequent layer. In certain embodiments, thethickness of each layer can be the same. In certain embodiments thethickness of each layer as formed can be from 0.5 millimeters (mm) to 5mm.

An object can be formed from a preset pattern, which can be determinedfrom a three-dimensional digital representation of the desired object asis known in the art and as described herein. Material can be joined orsolidified under computer control, for example, working from acomputer-aided design (CAD) model, to create the three-dimensionalobject.

The fused layers of powder bed fused objects can be of any thicknesssuitable for selective laser sintered processing. The individual layerscan be each, on average, preferably at least 50 micrometers (μm) thick,more preferably at least 80 μm thick, and even more preferably

of sintered layers are each, on

than 300 μm thick, and even

layers for some embodiments can be 50 to 500 μm, 80 to 300 μm, or 100 to200 μm thick. Three-dimensional objects produced from powdercompositions of the present technology using a layer-by-layer powder bedfusing processes other than selective laser sintering can have layerthicknesses that are the same or different from those described above.

“Polycarbonate” as used herein means a polymer or copolymer havingrepeating structural carbonate units of formula (1):

wherein at least 60 percent of the total number of R¹ groups arearomatic, or each R¹ contains at least one C₆₋₃₀ aromatic group.Specifically, each R¹ can be derived from a dihydroxy compound such asan aromatic dihydroxy compound of formula (2) or a bisphenol of formula(3), as follows:

In formula (2), each R^(h) is independently a halogen atom, for examplebromine, a C₁₋₁₀ hydrocarbyl group such as a C₁₋₁₀ alkyl, ahalogen-substituted C₁₋₁₀ alkyl, a C₆₋₁₀ aryl, or a halogen-substitutedC₆-10 aryl, and n is 0 to 4.

In formula (3), R^(a) and R^(b) are each independently a halogen, C₁₋₁₂alkoxy, or C₁₋₁₂ alkyl, and p and q are each independently integers of 0to 4, such that when p or q is less than 4, the valence of each carbonof the ring is filled by hydrogen. In certain embodiments, p and q areeach 0, or p and q are each 1, and R^(a) and R^(b) are each a C₁₋₃ alkylgroup, specifically methyl, disposed meta to the hydroxy group on eacharylene group. X^(a) is a bridging group connecting the twohydroxy-substituted aromatic groups, where the bridging group and thehydroxy substituent of each C₆ arylene group are disposed ortho, meta,or para (specifically para) to each other on the C₆ arylene group, forexample, a single bond, —O—, —S—, —S(O)—, —S(O)₂— (e.g., bisphenol-Spolycarbonate, polysulfone), —C(O)— (e.g., polyketone), or a C₁-18organic group, which can be cyclic or acyclic, aromatic or non-aromatic,and can further comprise heteroatoms such as halogens, oxygen, nitrogen,sulfur, silicon, or phosphorous. For example, X^(a) can be a substitutedor unsubstituted C₃₋₁₈ cycloalkylidene; a C₁₋₂₅ alkylidene of theformula —C(R^(c))(R^(d))— wherein R^(c) and R^(d) are each independentlyhydrogen, C₁₋₁₂ alkyl, C₁₋₁₂ cycloalkyl, C₇-12 arylalkyl, C₁-12heteroalkyl, or cyclic C₇-12 heteroarylalkyl; or a group of the formulaC(═R^(e))— wherein R^(e) is a divalent C₁₋₁₂ hydrocarbon group. Certainillustrative examples of dihydroxy compounds that can be used aredescribed, for example, in WO 2013/175448 A1, US 2014/0295363, and WO2014/072923.

Specific dihydroxy compounds include resorcinol,2,2-bis(4-hydroxyphenyl) propane (“bisphenol A” or “BPA”),3,3-bis(4-hydroxyphenyl) phthalimidine,2-phenyl-3,3′-bis(4-hydroxyphenyl) phthalimidine (also known as N-phenylphenolphthalein bisphenol, “PPPBP”, or3,3-bis(4-hydroxyphenyl)-2-phenylisoindolin-1-one),1,1-bis(4-hydroxy-3-methylphenyl)cyclohexane, and1,1-bis(4-hydroxy-3-methylphenyl)-3,3,5-trimethylcyclohexane (isophoronebisphenol).

“Polycarbonate” as used herein also includes copolymers comprisingcarbonate units and ester units (“poly(ester-carbonate)s”, also known aspolyester-polycarbonates). Poly(ester-carbonate)s further contain, inaddition to recurring carbonate chain units of formula (1), repeatingester units of formula (4):

wherein J is a divalent group derived from a dihydroxy compound (whichincludes a reactive derivative thereof), and can be, for example, aC₂₋₁₀ alkylene, a C₆-20 cycloalkylene a C₆-20 arylene, or apolyoxyalkylene group in which the alkylene groups contain 2 to 6 carbonatoms, specifically, 2, 3, or 4 carbon atoms; and T is a divalent groupderived from a dicarboxylic acid (which includes a reactive derivativethereof), and can be, for example, a C₂-20 alkylene, a C₆-20cycloalkylene, or a C₆₋₂₀ arylene. Copolyesters containing a combinationof different T or J groups can be used. The polyester units can bebranched or linear.

Specific dihydroxy compounds include aromatic dihydroxy compounds offormula (2) (e.g., resorcinol), bisphenols of formula (3) (e.g.,bisphenol A), a C₁₋₈ aliphatic diol such as ethane diol, n-propane diol,i-propane diol, 1,4-butane diol, 1,6-cyclohexane diol,1,6-hydroxymethylcyclohexane, or a combination comprising at least oneof the foregoing dihydroxy compounds. Aliphatic dicarboxylic acids thatcan be used include C₆₋₂₀ aliphatic dicarboxylic acids (which includesthe terminal carboxyl groups), specifically linear C₈₋₁₂ aliphaticdicarboxylic acid such as decanedioic acid (sebacic acid); and alpha,omega-C_(a) dicarboxylic acids such as dodecanedioic acid (DDDA).Aromatic dicarboxylic acids that can be used include terephthalic acid,isophthalic acid, naphthalene dicarboxylic acid, 1,6-cyclohexanedicarboxylic acid, or a combination comprising at least one of theforegoing acids. A combination of isophthalic acid and terephthalic acidwherein the weight ratio of isophthalic acid to terephthalic acid is91:9 to 2:98 can be used.

Specific ester units include ethylene terephthalate units, n-propyleneterephthalate units, n-butylene terephthalate units, ester units derivedfrom isophthalic acid, terephthalic acid, and resorcinol (ITR esterunits), and ester units derived from sebacic acid and bisphenol A. Themolar ratio of ester units to carbonate units in thepoly(ester-carbonate)s can vary broadly, for example 1:99 to 99:1,specifically, 10:90 to 90:10, more specifically, 25:75 to 75:25, or from2:98 to 15:85.

The polycarbonates can have an intrinsic viscosity, as determined inchloroform at 25° C., of 0.3 to 1.5 deciliters per gram (dl/gm),specifically 0.45 to 1.0 dl/gm. The polycarbonates can have a weightaverage molecular weight of 5,000 to 200,000 Daltons, specifically15,000 to 100,000 Daltons, as measured by gel permeation chromatography(GPC), using a crosslinked styrene-divinylbenzene column and calibratedto polycarbonate references. GPC samples are prepared at a concentrationof 1 mg per ml (mg/ml), and are eluted at a flow rate of 1.5 ml perminute.

In certain embodiments, the method of preparing a partially crystallinepolycarbonate powder comprises dissolving an amorphous polycarbonate ina polar aprotic solvent such as dimethyl sulfoxide (DMSO) at atemperature above room temperature. Room temperature is understood to beabout 20° C. (68° F.); as such, the amorphous polycarbonate can bedissolved in DMSO at a temperature above about 20° C. The amorphouspolycarbonate is soluble in the DMSO solvent and thus a polycarbonatesolution is formed. In general, the solution can be prepared at atemperature above room temperature so that the amount of dissolvedamorphous polycarbonate can be considered supersaturated at roomtemperature. Mixing of amorphous polycarbonate into DMSO solvent can becarried out in-line or batch. The process can readily be carried out atmanufacturing scale. Upon cooling to room temperature (e.g., about 20°C.), the dissolved amorphous polycarbonate begins to crystallize andprecipitate out of the DMSO solvent resulting in the precipitation of apartially crystalline polycarbonate precipitate. It is further possiblethat when the precipitation occurs under high shear mixing conditions,the formation of an increased percentage of crystalline polycarbonateparticles occurs while simultaneously preventing formation of firmlyagglomerated polycarbonate particles. It has been found, for example,that agglomerates can be readily broken by crushing, high speed mixing,or other low- or medium-force shearing processes.

Following precipitation, the DMSO solvent is removed and the partiallycrystalline polymer powder can be dried by heat with or without vacuum.The resulting crystalline polycarbonate powder can have a higherpercentage of particles having a particle size of less than 150micrometers, as well as a relatively narrow particle size distribution.The recovered DMSO solvent can be reused to begin the process anew bydissolving additional amorphous polycarbonate. This is unlike othermethods that use one or more solvents that are mixed with non-solventsto precipitate crystalline polycarbonate powder. Such mixtures ofsolvents and non-solvents cannot be readily reused.

As provided herein, amorphous polycarbonate is dissolved in DMSOsolvent. For example, the amorphous polycarbonate can be dissolved inDMSO under conditions that result in a supersaturated solution ofpolycarbonate, where changing conditions (e.g., changing temperature ofthe solution) result in precipitation of partially crystallinepolycarbonate powder therefrom. In certain embodiments, the solvent caninclude DMSO as well as one or more other polar aprotic solvents. Incertain embodiments, the solvent can consist essentially of DMSO, whereno other components are present that materially affect thecrystallization of polycarbonate; e.g., no non-solvents are present, asdescribed by U.S. Pub. No. 2018/0244863. In certain embodiments, thesolvent can consist of DMSO, where there are substantially no othersolvents present based upon the purity levels attainable in the art withrespect to DMSO. That is, the solvent can be substantially 100% DMSO. Itis further noted that upon precipitating partially crystallinepolycarbonate powder from a solution of amorphous polycarbonate andDMSO, a portion of the solubilized amorphous polycarbonate can remain insolution. Separation of the precipitated partially crystallinepolycarbonate powder from the remainder of the solution therefore leavesa solution of DMSO with a portion of solubilized amorphous polycarbonatethat can be reused to again dissolve more amorphous polycarbonate. Inthe repeat use of the DMSO (including the already dissolved portion ofamorphous polycarbonate), less amorphous polycarbonate may need to beadded to achieve a supersaturated state, for example, where changingfrom the first temperature to the lower second temperature results inanother precipitation of partially crystalline polycarbonate powder.

In certain embodiments, the partially crystalline polycarbonate powderhas a D85 particle size of less than 150 micrometers, specifically, aD90 particle size of less than 150 micrometers. In certain embodiments,the partially crystalline polycarbonate powder has a D93 particle sizeof less than 150 micrometers, in which 93% of the partially crystallinepolycarbonate powder has a particle size of less than 150 μm. Certainembodiments include where the partially crystalline polycarbonate powderhas a D90 particle size of less than 150 μm. A partially crystallinepolycarbonate powder in which 100% of the particles have a size of lessthan 150 micrometers can also be produced by this method.

The partially crystalline polycarbonate powder can also have an averageparticle diameter of less than or equal to 100 μm. Specifically, thepartially crystalline polycarbonate powder can have an average particlediameter of 10 μm to 100 μm. The average particle diameter of thepartially crystalline polycarbonate powder can also be less than orequal to 100 μm, or include an average particle diameter of between 0 to100 μm.

In certain embodiments, the partially crystalline polycarbonate powderhas a percent crystallinity of at least 20%, for example 20% to 80%,specifically, at least 25%, for example 25% to 60%, more specifically atleast 27%, for example 27% to 40%. The partially crystallinepolycarbonate powder can also have 25% to 30% crystallinity. Embodimentsfurther include 25% to 35% crystallinity.

In certain embodiments, a method of preparing an article comprisesproviding a powder composition comprising the partially crystallinepolycarbonate powder, and using a powder bed fusing process with thepowder composition to form a three-dimensional object. The at least onepartially crystalline polycarbonate powder can have a D50 particle sizeof less than 150 micrometers in diameter and is made by above-describedmethods. Embodiments include where the partially crystallinepolycarbonate powder has a D90 particle size of less than 150 μm, anaverage particle diameter of less than or equal to 100 μm, or an averageparticle diameter of between 0 to 100 μm, and at least 20%crystallinity, or at least 25% crystallinity, or 25 to 35%crystallinity. The partially crystalline polycarbonate powder can bemade as described herein by converting an amorphous polycarbonate to thecrystalline polycarbonate powder. The conversion of the amorphouspolycarbonate includes dissolving the amorphous polycarbonate in DMSOsolvent to form a solution above room temperature, cooling the solutionto room temperature to form a precipitate including partiallycrystalline polycarbonate powder, removing the solvent from theprecipitate, drying the precipitate, and recovering the crystallinepolycarbonate powder.

The partially crystalline polycarbonate powder can be used as the solecomponent in the powder composition and applied directly in a powder bedfusing step. Alternatively, the partially crystalline polycarbonatepowder can first be mixed with other polymer powders, for example,another crystalline polymer or an amorphous polymer, or a combination ofa partially crystalline polymer and an amorphous polymer. The powdercomposition used in the powder bed fusing can include between 50 wt % to100 wt % of the partially crystalline polycarbonate powder, based on thetotal weight of all polymeric materials in the powder composition.

The partially crystalline polycarbonate powder can also be combined withone or more additives/components to make a powder useful for powder bedfusing methods. Such optional components can be present in a sufficientamount to perform a particular function without adversely affecting thepowder composition performance in powder bed fusing or the objectprepared therefrom. Optional components can have an average particlediameter which falls within the range of the average particle diametersof the partially crystalline polycarbonate powder or an optional flowagent. If necessary, each optional component can be milled to a desiredparticle size and/or particle size distribution, which can besubstantially similar to the partially crystalline polycarbonate powder.Optional components can be particulate materials and include organic andinorganic materials such as fillers, flow agents, and coloring agents.Still other additional optional components can also include, forexample, toners, extenders, fillers, colorants (e.g., pigments anddyes), lubricants, anticorrosion agents, thixotropic agents, dispersingagents, antioxidants, adhesion promoters, light stabilizers, organicsolvents, surfactants, flame retardants, anti-static agents,plasticizers a combination comprising at least one of the foregoing. Yetanother optional component also can be a second polymer that modifiesthe properties of the partially crystalline polycarbonate. In certainembodiments, each optional component, if present at all, can be presentin the powder composition in an amount of 0.01 wt % to 30 wt %, based onthe total weight of the powder composition. The total amount of alloptional components in the powder composition can range from 0 up to 30wt % based on the total weight of the powder composition.

It is not necessary for each optional component to melt during thepowder bed fusing process; e.g., a laser sintering process. However,each optional component can be selected to be compatible with thepartially crystalline polycarbonate polymer in order to form a strongand durable object. The optional component, for example, can be areinforcing agent that imparts additional strength to the formed object.Examples of the reinforcing agents include one or more types of glassfibers, carbon fibers, talc, clay, wollastonite, glass beads, andcombinations thereof.

The powder composition can optionally contain a flow agent. Inparticular, the powder composition can include a particulate flow agentin an amount of 0.01 wt % to 5 wt %, specifically, 0.05 wt % to 1 wt %,based on the total weight of the powder composition. In certainembodiments, the powder composition comprises the particulate flow agentin an amount of 0.1 wt % to 0.25 wt %, based on the total weight of thepowder composition. The flow agent included in the powder compositioncan be a particulate inorganic material having a median particle size of10 μm or less, and can be chosen from a group consisting of hydratedsilica, amorphous alumina, glassy silica, glassy phosphate, glassyborate, glassy oxide, titania, talc, mica, fumed silica, kaolin,attapulgite, calcium silicate, alumina, magnesium silicate, andcombinations thereof. The flow agent can be present in an amountsufficient to allow the partially crystalline polycarbonate polymer toflow and level on the build surface of the powder bed fusing apparatus(e.g., a laser sintering device). In certain embodiments the flow agentincludes fumed silica.

Another optional component is a coloring agent, for example a pigment ora dye, like carbon black, to impart a desired color to the object. Thecoloring agent is not limited, as long as the coloring agent does notadversely affect the composition or an object prepared therefrom, andwhere the coloring agent is sufficiently stable to retain its colorunder conditions of the powder bed fusing process and exposure to heatand/or electromagnetic radiation; e.g., a laser used in a sinteringprocess.

Still further additives include, for example, toners, extenders,fillers, colorants (e.g., pigments and dyes), lubricants, anticorrosionagents, thixotropic agents, dispersing agents, antioxidants, adhesionpromoters, light stabilizers, organic solvents, surfactants, flameretardants, anti-static agents, plasticizers, and combinations of such.

Still another optional component also can be a second polymer thatmodifies the properties of the partially crystalline polycarbonatepowder.

The powder composition is a fusible powder composition and can be usedin a powder bed fusing process such as selective laser sintering. Anexample of a selective laser sintering system for fabricating a partfrom a fusible powder composition, and in particular for fabricating thepart from the fusible crystalline polycarbonate powder disclosed herein,can be described as follows. One thin layer of powder compositioncomprising the partially crystalline polycarbonate powder is spread overthe sintering chamber. The laser beam traces the computer-controlledpattern, corresponding to the cross-section slice of the CAD model, tomelt the powder selectively which has been preheated to slightly belowits melting temperature. After one layer of powder is sintered, thepowder bed piston is lowered with a predetermined increment (typically100 μm), and another layer of powder is spread over the previoussintered layer by a roller. The process then repeats as the laser meltsand fuses each successive layer to the previous layer until the entireobject is completed. Three-dimensional objects comprising a plurality offused layers can thus be made using the partially crystallinepolycarbonate powder described herein.

The present technology provides certain benefits and advantages. Oneadvantage is the use of a single solvent in preparing the partiallycrystalline polycarbonate powder, which facilitates solvent recovery andreuse thereof. Another advantage is that amorphous polycarbonate can betransformed into a polycarbonate powder having optimized crystallinityand optimized particle size distribution. Yet another advantage is thatthe partially crystalline polycarbonate powder provides improved powderbed fusion performance. Additive manufacturing processes that employfusion of a powder bed, including selective laser sintering (SLS), multijet fusion (MJF), high speed sintering (HSS), and electrophotographic3D-printing, can therefore benefit by forming and using partiallycrystalline polycarbonate powder produced as described herein.

The following Examples further illustrate the above concepts.

Example 1

An illustrative embodiment of the process for making pulverulentpolycarbonate suitable for additive manufacturing is as follows. To a5-L four-neck round-bottom flask fitted with an overhead stirrer wasadded 1 kg polycarbonate (Lupoy 1303EP-22, MW=ca. 38,000 Da) and 3 LDMSO (99.7%, Acros Organics). The solvent was sparged and the flaskflushed with a nitrogen atmosphere for 20 minutes. The mixture washeated with an electric mantle to 160° C. with stirring at a rate of 200rpm to yield a solution of polycarbonate in DMSO. The mantle was removedto allow the reactor temperature to cool at a rate of 1° C./min whilecontinuing to stir at 200 rpm. The polycarbonate precipitated betweenabout 70° C. and about 80° C. The thick slurry was removed from thereactor and poured into a 50 μm nylon mesh bag nested inside of a 100 μmnylon mesh bag of equivalent dimensions. The DMSO was separated bysqueezing the bags. The residual powder was washed 3×4 L of water: thefirst for 30 min., the second for 15 hrs., and the third for 4 hrs. Thepowder slurry was filtered and dried at 120° C. for 16 hrs., followed bysieving sequentially through 250 μm and 180 μm sieves.

Density and Flowability. Average bulk density of pulverulentpolycarbonate prepared in this embodiment was 0.42 g/cm³. Average tapdensity was 0.52 g/cm³ (average Hausner ratio=1.26, Carr's index 0.20).Flowability was determined using a cone with a 10 mm nozzle diameter,and has an average value of 2.58 g/sec.

Particle size, shape and distribution (PSSD). PSSD was determined inwater using a Microtrac 53500 instrument. D₉₀=67.8 μm; D₅₀=37.7 μm;D₁₀=16.8 μm. Sphericity data is as shown in Table 1.

TABLE 1 >0.65 97.03% >0.75 89.64% >0.85 64.43% >0.90 28.70% >0.95 7.01%

Molecular weight. GPC samples were prepared at a concentration of 2mg/mL tetrahydrofuran (THF), and are eluted at a flow rate of 1 mL/min.on a Waters GPC instrument with a Styragel HR4 5-μm 7.8×300 mm (THF)Column and a 2414 Refractive Index Detector. The peak molecular weight(M_(P)) of the raw polycarbonate=38093 Da; M_(P) of pulverulentpolycarbonate=29900 Da.

Scanning Electron Micrography (SEM). SEM images reveal spheroidal,partially agglomerated particles of a typical size in agreement withPSSD results.

Differential Scanning calorimetry (DSC) and Crystallinity. The DSC wasperformed on a TA Instruments DSC 250 instrument scanning at 20° C./min.and is shown in FIG. 3 . Onset of melting occurred at 208.88° C., andpeaked at 236.39° C. Upon cooling, a glass transition appeared at 142°C., and again upon secondary heating at 147° C., after which no meltingbehavior was observed.

The percent crystallinity of semi-crystalline pulverulent polycarbonatewas estimated by measuring the enthalpy of fusion in the melting peak(31.407 J/g) and comparing it with the reference value for the enthalpyof fusion for 100% crystalline polycarbonate, reported as 134 J/g in theliterature (K. Varadarajan, et al., J. Polym. Sci. Polym. Phys. 1982,20(1), 141-154). The estimated crystallinity of semi-crystallinepolycarbonate was therefore 23.4%.

SLS Printing of Pulverulent Polycarbonate. The pulverulent polycarbonatewas utilized in the laser sintering process on a Farsoon ST252P lasersintering system. Three kilograms of material was loaded into the feedpiston of the machine and settled into the piston achieving the optimaltapped density using a cement vibrator. Under an inert nitrogenatmosphere, material was moved from the feed piston to the part pistonin a layerwise fashion using a counter-rotating roller at layerthicknesses of 0.080 mm. Layers were laid at 90 s intervals in order toallow for sufficient thermal absorption from near-IR heaters, duringwhich time the temperature of the feed piston ramped from 60° C. to 180°C. and the part bed temperature ramped from 60° C. to 207° C. Once thepart bed temperature reached the set point of 207° C., part areas wereexposed using the scanning system parameters shown in Table 2 in orderto melt selected areas into solid parts.

TABLE 2 Laser spot size (μm) 450 Fill scan speed (mm/s) 10,160 Fill scanspacing (mm) 0.28 Fill laser power (W) 30

Parts produced included thin discs, crosses, “window” test coupons, andASTM D638 Type IV tensile bars. Parts featured a slight yellow tint, butwere mostly translucent and lacked the opaque appearance of typicallaser sintering materials.

Example 2

An illustrative embodiment of the process for making pulverulentpolycarbonate suitable for additive manufacturing is as follows. To a20-L Reactor fitted with an overhead stirrer was added 4.0 kgpolycarbonate (Lexan 121R 112) and 15.73 L DMSO (99.7%, Acros Organics).The solvent was sparged and the flask flushed with an argon atmospherefor 4 hours. The mixture was heated with an oil jacket to 160° C. withstirring at a rate of 180 rpm to yield a solution of polycarbonate inDMSO. The reactor was allowed cool at a rate of 0.1-0.2° C./min whilecontinuing to stir at 180 rpm. The polycarbonate precipitated betweenabout 70° C. and about 80° C. The thick slurry was removed from thereactor and poured into a 50 μm nylon mesh bag nested inside of a 100 μmnylon mesh bag of equivalent dimensions. The DMSO was separated bysqueezing the bags. The residual powder was soaked in 1×30 L of waterfor 3 days. This was removed by using the aforementioned bags. Theresidual powder was soaked in 1×10 L of Methanol for 2 hours andseparated using 5 μm filter paper in a 20 L vacuum filter. The powderwas dried at 120° C. for 33 hrs., followed by sieving sequentiallythrough 250 μm and 180 μm sieves.

Particle size and distribution (PSD). PSD was determined in air using aMicrotrac S3500 instrument. D₉₀=22.48 μm; D₅₀=14.96 μm; D₁₀=10.93 μm.Sphericity data is as follows:

Differential Scanning calorimetry (DSC) and Crystallinity. The DSC wasperformed on a TA Instruments DSC 250 instrument scanning at 20° C./min.and is shown in FIG. 3 . Onset of melting occurred at 207.56° C., andpeaked at 241.28° C.

The percent crystallinity of semi-crystalline pulverulent polycarbonatewas estimated by measuring the enthalpy of fusion in the melting peak(31.377 J/g) and comparing it with the reference value for the enthalpyof fusion for 100% crystalline polycarbonate, reported as 134 J/g in theliterature (K. Varadarajan, et al., J. Polym. Sci. Polym. Phys. 1982,20(1), 141-154). The estimated crystallinity of semi-crystallinepolycarbonate was therefore 23.4%.

SLS Printing of Pulverulent Polycarbonate. The pulverulent polycarbonatewas utilized in the laser sintering process on a Farsoon ST252P lasersintering system. Two and one half kilograms of material was loaded intothe feed piston of the machine and settled into the piston achieving theoptimal tapped density using a cement vibrator. Under an inert nitrogenatmosphere, material was moved from the feed piston to the part pistonin a layerwise fashion using a counter-rotating roller at layerthicknesses of 0.061 mm. Layers were laid at 90 s intervals in order toallow for sufficient thermal absorption from near-IR heaters, duringwhich time the temperature of the feed piston ramped from 60° C. to 180°C. and the part bed temperature ramped from 60° C. to 207° C. Once thepart bed temperature reached the set point, it was lowered to 205.5° C.as the part bed started to crack, part areas were exposed using thescanning system parameters in Table 3 in order to melt selected areasinto solid parts.

TABLE 3 Laser spot size (μm) 450 Fill scan speed (mm/s) 10,160 Fill scanspacing (mm) 0.20 Fill laser power (W) 60 Number of scans 3 Layerinterval (s) 23

Parts produced included thin discs, crosses, “window” test coupons, andASTM D638 Type IV tensile bars. Parts featured a slight yellow tint, butwere mostly translucent and lacked the opaque appearance of typicallaser sintering materials.

Example 3

An illustrative embodiment of the process for making pulverulentpolycarbonate suitable for additive manufacturing is as follows. To a20-L Reactor fitted with an overhead stirrer was added 3.21 kgpolycarbonate (Lupoy 1080C 70, MW=ca. 30,000 Da) and 13.76 L DMSO(99.7%, Acros Organics) [A second batch consisting of 3.00 kgpolycarbonate (Lupoy 1080C 70) and 12.96 L DMSO (99.7%, Acros Organics)was performed alongside this one]. The solvent was sparged and thereactor flushed with an argon atmosphere for 3 hours. The mixture washeated with an oil jacket to 160° C. with stirring at a rate of 180 rpmto yield a solution of polycarbonate in DMSO. The reactor was allowedcool at a rate of 0.1-0.2° C./min while continuing to stir at 180 rpm.The polycarbonate precipitated between about 70° C. and about 80° C. Theslurry was removed from the reactor, combined with the second batch, andpoured into a 20 L vacuum filter flask with a 4 μm filter paper. 15 L ofDMSO was recovered using this method. The residual powder was processedusing 140 L of DI water and 20 L of acetone as follows: soaked in 2×15 Lof water for 1 day; filtered and soaked with 1×25 L of water for 1 day;filtered, washed with 2×20 L of water, and soaked in 25 L of water for 1day; filtered, washed with 1×20 L of water and 1×20 L of acetone. Thepowder was dried at 110° C. for 72 hrs., followed by a 250 μm sieveproviding 4.5 kg of powder.

Density and Flowability. Average bulk density of pulverulentpolycarbonate prepared in this embodiment was 0.42 g/cm³. Average tapdensity was 0.48 g/cm³ (average Hausner ratio=1.15, Carr's index 0.12).Flowability was determined using a cone with a 15 mm nozzle diameter,and has an average value of 8.93 g/sec.

Particle size distribution (PSD). PSD was determined in air using aMicrotrac S3500 instrument. D₉₀=101.5 μm; D₅₀=69.56 μm; D₁₀=45.69 μm.

Molecular weight. GPC samples were prepared at a concentration of 2mg/mL tetrahydrofuran (THF), and are eluted at a flow rate of 1 mL/min.on a Waters GPC instrument with a Styragel HR4 5-μm 7.8×300 mm (THF)Column and a 2414 Refractive Index Detector. The peak molecular weight(M_(P)) of the raw polycarbonate=30318 Da.

Scanning Electron Micrography (SEM). SEM images reveal spheroidal,partially agglomerated particles of a typical size in agreement with PSDresults.

Differential Scanning calorimetry (DSC) and Crystallinity. The DSC wasperformed on a TA Instruments DSC 250 instrument scanning at 20° C./min.and is shown in FIG. 3 . Onset of melting occurred at 196.67° C., andpeaked at 233.97° C. Upon secondary heating, a glass transition occurredat 138.84° C., after which no melting behavior was observed.

The percent crystallinity of semi-crystalline pulverulent polycarbonatewas estimated by measuring the enthalpy of fusion in the melting peak(31.407 J/g) and comparing it with the reference value for the enthalpyof fusion for 100% crystalline polycarbonate, reported as 134 J/g in theliterature (K. Varadarajan, et al., J. Polym. Sci. Polym. Phys. 1982,20(1), 141-154). The estimated crystallinity of semi-crystallinepolycarbonate was therefore 26.9%.

SLS Printing of Pulverulent Polycarbonate. The pulverulent polycarbonatewas utilized in the laser sintering process on a Farsoon ST252P lasersintering system. Four and one half kilograms of material was loadedinto the feed piston of the machine and settled into the pistonachieving the optimal tapped density using a cement vibrator. Under aninert nitrogen atmosphere, material was moved from the feed piston tothe part piston in a layerwise fashion using a counter-rotating rollerat layer thicknesses of 0.102 mm. Layers were laid at 90 s intervals inorder to allow for sufficient thermal absorption from near-IR heaters,during which time the temperature of the feed piston ramped from 60° C.to 200° C. and the part bed temperature ramped from 60° C. to 219° C.Once the part bed temperature reached the set point of 219° C., partareas were exposed using the scanning system parameters shown in Table 4in order to melt selected areas into solid parts.

TABLE 4 Laser spot size (μm) 450 Fill scan speed (mm/s) 10,160 Fill scanspacing (mm) 0.20 Fill laser power (W) 35 Number of scans 2 Layerinterval (s) 30

Parts produced included thin discs, large cubes, and ASTM D638 Type IVtensile bars. Parts featured a slight yellow tint, but were mostlytranslucent and lacked the opaque appearance of typical laser sinteringmaterials.

Example 4

30 g of Lexan 121 polycarbonate was dissolved in 100 ml of acetophenone.The mixture was placed in a 300 ml Erlenmeyer flask and stirred andheated on a magnetic hot plate to 182° C. At this temperature, thepolycarbonate was observed to be fully dissolved. The heater was turnedoff and the solution was allowed to cool while stirring. The solutionwas visually cloudy when observed at approximately 52° C. The solutionwas held at ambient conditions (approximately 20° C.) overnight, forapproximately 15 hours. 200 ml of acetone was added to thin out thesolution before filtering via vacuum filtration. The solids that wereseparated from the solution were dried by placing them in a ventilatedlab hood overnight.

Process

An illustrative process of making pulverulent polycarbonate for additivemanufacturing and other applications comprises: adding the polycarbonateto a reactor vessel containing a solvent which may be selected from agroup including: dimethyl sulfoxide (DMSO); acyclic and cyclic ketonessuch as cyclopentanone, cyclohexanone, or acetophenone; acyclic andcyclic secondary amides (e.g., N-methylpyrrolidinone (NMP) orN,N-dimethylformamide (DMF)); acyclic and cyclic esters(γ-butyrolactone); halogenated hydrocarbons (e.g., dichloromethane);anisole; or phenols (e.g., m-cresol); optionally mixing in additivesubstances (e.g., inorganic oxide(s), organic compounds, carbonmicrofibers, glass microfibers, and/or secondary polymers) for thepurpose(s) of particle nucleation, particle dispersion, IR absorption,mineralization and strengthening, flame retardancy, and/or coloration;applying an inert atmosphere to the vessel. agitating the mixture;raising the temperature in the container; forming a solution ofpolycarbonate; cooling the solution to a precipitation temperature ofthe polycarbonate; precipitating the polycarbonate in powder form fromthe solution; removing the polycarbonate powder slurry from the reactor;separating the polycarbonate from the solvent by filtration; washing thepolycarbonate powder with a quantity of wash solvent (e.g., water and/ora volatile organic solvent such as alcohol, ketone, ether, ester orhydrocarbon in which polycarbonate does not significantly dissolve) toremove the reprecipitation solvent; and drying the polycarbonate byheating above 150° C., preferably above 175° C., and most preferablyabove 195° C. but not above 205° C., and preferably under reducedpressure.

It is believed that the presence of a polar solvent exhibiting effectiveintermolecular interactions with the polar functional groups in thepolycarbonate chains facilitates organization of the polymer chains intocrystalline domains in the precipitation process.

A variety of methods to chemically precipitate the above-identifiedpolymers may be employed. One skilled in the art will appreciate, basedon illustrative methods described below, that other precipitationmethods may be employed in the embodiments though they are notexplicitly disclosed herein.

Another illustrative method of making the powder from polycarbonate mayinclude evaporation limited coalescence and anti-solvent precipitation.

The term “agitating the mixture” refers to methods of stirring thecomponents in a liquid or slurried mixture under conditions in whichshear forces are generated, creating patterns of flow and turbulence,generally using an impellor that rotates inside a stator. Once theimpellor has drawn mixture in, it subjects the mixture to sudden changesof direction and acceleration such that the mixture contacts the wall ofthe stator with centrifugal force, or is forced through the holes in thestator under pressure and speed, in a final disintegrating change ofdirection and acceleration. In exemplary embodiments of high shearmixing conditions, mixing comprises operating at speeds of 50 rotationsper minute (rpm) to 500 rpm. Agitation can be achieved with anycommercially available mixers; for example, a mixer such as a Hei-Torque200 reactor stirring motor can be used.

It is appreciated that the rotation rate of the stirrer, precipitationtemperature, and time can be modified to potentially affect the particlesize of the resulting polycarbonate powder. It is also appreciated thatthe powder may be reprecipitated.

It is further appreciated that the polycarbonate may also be mixed indifferent ratios and particle sizes. This may have the effect ofchanging or controlling the properties of the resulting pulverulentpolycarbonate. It is further contemplated that the polycarbonate may bedeveloped in powdered form through other methods of chemicalprecipitation.

Melting point and enthalpy may be determined using differential scanningcalorimetry (DSC); for example, a TA Instruments Discovery Series DSC250.

Powder flow may be measured using Method A of ASTM D 1895.

Young's modulus of elasticity and tensile strength maybe determinedpursuant to the ASTM D 790 standard.

Scanning electron microscopy was performed using a JEOL instrumentoperating in low vacuum secondary electron detection (LVSED) mode.

The process for modifying the produced pulverulent polycarbonatematerial for additive manufacturing may comprise: adding at least onecompatible filler to the polycarbonate, wherein the fillers are eitherorganic or inorganic; at least one filler being selected from the groupconsisting of glass, metal, or ceramic particles, pigments, titaniumdioxide particles, and carbon black particles; particle size of at leastone filler being about equal to or less than particle sizes of thepolycarbonate; the particle sizes of at least one filler does not varymore than about 15-20 percent of an average particle size of thepolycarbonate; at least one filler is less than about 3% by weight ofthe polycarbonate; a flow agent being incorporated into the powderedpolycarbonate; the flow agent being selected from at least one of afumed silicas, calcium silicates, alumina, amorphous alumina, magnesiumsilicates, glassy silicas, hydrated silicas, kaolin, attapulgite, glassyphosphates, glassy borates, glassy oxides, titania, talc, pigments, andmica; the flow agent having a particle size of about 10 microns or less;the flow agent does not significantly alter the glass transitiontemperature of the polycarbonate; the flow agent is present in an amountless than about 5% by weight of polycarbonate.

Disclosed herein also are methods for powder bed fusing a powdercomposition, including the partially crystalline polycarbonate powder,to form a three-dimensional article. The spheroidal shape of the polymerpowder particles results in good flowability of the partiallycrystalline polycarbonate powder, and thus a smooth and dense powder bedcan be formed allowing for optimum precision and density of the sinteredpart. Also, the partially crystalline nature of the polymeric materialallows for ease of processing.

“Powder bed fusing” or “powder bed fusion” includes all laser sinteringand all selective laser sintering processes as well as other powder bedfusing technologies as defined by ASTM F2792-12a. For example, sinteringof the powder composition can be accomplished via application ofelectromagnetic radiation other than that produced by a laser, with theselectivity of the sintering achieved, for example, through selectiveapplication of inhibitors, absorbers, susceptors, or the electromagneticradiation (e.g., through use of masks or directed laser beams). Anyother suitable source of electromagnetic radiation can be used,including, for example, infrared radiation sources, microwavegenerators, lasers, radiative heaters, lamps, or a combination thereof.

Also included herein are all three-dimensional products made by powderbed fusing these powder compositions. After a layer-by-layer manufactureof an article of manufacture, the article can exhibit excellentresolution, durability, and strength. These articles of manufacture canhave a wide variety of uses, including as prototypes and as end productsas well as molds for end products.

In some embodiments of the methods, a plurality of layers is formed in apreset pattern by an additive manufacturing process. “Plurality”, asused in the context of additive manufacturing, includes five or morelayers, or twenty or more layers. The maximum number of layers can varygreatly, determined, for example, by considerations such as the size ofthe article being manufactured, the technique used, the capabilities ofthe equipment used, and the level of detail desired in the finalarticle.

As used herein, “layer” is a term of convenience that includes anyshape, regular or irregular, having at least a predetermined thickness.In some embodiments, the size and configuration of two dimensions arepredetermined, and on some embodiments, the size and shape of allthree-dimensions of the layer is predetermined. The thickness of eachlayer can vary widely depending on the additive manufacturing method. Insome embodiments, the thickness of each layer as formed differs from aprevious or subsequent layer. In some embodiments, the thickness of eachlayer is the same. In some embodiments the thickness of each layer asformed is 0.05 millimeters (mm) to 5 mm.

The preset pattern can be determined from a 3D digital representation ofthe desired article as is known in the art and described in furtherdetail below.

The fused layers of powder bed fused articles can be of any thicknesssuitable for selective laser sintered processing. The individual layerscan be each, on average, preferably at least 100 μm thick, more preferably at least 80 μm thick, and even more preferably at least 50 μmthick. In a preferred embodiment, the plurality of sintered layers areeach, on average, preferably less than 500 μm thick, more preferablyless than 300 μm thick, and even more preferably less than 200 μm thick.Thus, the layers for some embodiments can be 50 to 500 μm, 80 to 300 μm,or 100 to 200 μm thick. Three-dimensional articles produced from powdercompositions of the invention using a layer-by-layer powder bed fusingprocesses other than selective laser sintering can have layerthicknesses that are the same or different from those described above.

Powder-based 3D-printing includes a part bed and feed mechanism. Thispart bed is generally at a steady temperature before it is subjected toan energy source. That energy source is raised until a fusiontemperature is reached. The pulverulent polycarbonate may be placed in afeeder at a start temperature. During operation additional polycarbonateis placed on top of the original polycarbonate which cools and needs tobe raised again. It is believed that only the portion of polycarbonatethat is directly subjected to energy will be melted and not thesurrounding polycarbonate.

For purposes of this disclosure, an “operating window” is defined by thetypical range between the melting and the recrystallization (or glasstransition) temperatures. Semi-crystalline polycarbonates possess adefinitive melting point, allowing for the establishment of an operatingtemperature near the melting point of the polycarbonate in SLS, MJF,HSS, and possibly electrophotography 3D-printing applications. Thiswell-defined melting behavior allows for an operating window that keepsthe rest of the material unmelted, such as even in the presence of alaser or IR heater used during 3D-printing in solid form. The unmeltedsolid material can then act as a supporting structure for the moltenpolycarbonate.

Example embodiments are provided so that this disclosure will bethorough, and will fully convey the scope to those who are skilled inthe art. Numerous specific details are set forth such as examples ofspecific components, devices, and methods, to provide a thoroughunderstanding of embodiments of the present disclosure. It will beapparent to those skilled in the art that specific details need not beemployed, that example embodiments may be embodied in many differentforms, and that neither should be construed to limit the scope of thedisclosure. In some example embodiments, well-known processes,well-known device structures, and well-known technologies are notdescribed in detail. Equivalent changes, modifications and variations ofsome embodiments, materials, compositions and methods can be made withinthe scope of the present technology, with substantially similar results.

1. A method of preparing a partially crystalline polycarbonate powder,the method comprising: dissolving an amorphous polycarbonate in a polaraprotic solvent to form a first solution of solubilized polycarbonate ata first temperature; and cooling the first solution to a secondtemperature, the second temperature being lower than the firsttemperature, wherein a portion of the solubilized polycarbonateprecipitates from the first solution to form a second solution comprisedof precipitated partially crystalline polycarbonate powder and adissolved remaining portion of polycarbonate in the solvent.
 2. Themethod of claim 1, further comprising separating the precipitatedpartially crystalline polycarbonate powder from the second solutionleaving a remaining second solution comprised of the aprotic solvent anddissolved remaining portion of polycarbonate in the solvent.
 3. Themethod of claim 2, further comprising drying the separated partiallycrystalline polycarbonate powder.
 4. The method of claim 2, furthercomprising repeating the dissolving step using the remaining secondsolution as the polar aprotic solvent and repeating the cooling step toform the second solution including another partially crystallinepolycarbonate powder.
 5. The method of claim 1, wherein the polaraprotic solvent includes dimethyl sulfoxide.
 6. The method of claim 1,wherein the polar aprotic solvent consists essentially of dimethylsulfoxide.
 7. The method of claim 1, wherein the dissolving stepincludes heating the amorphous polycarbonate in the polar aproticsolvent to form the first solution of solubilized polycarbonate at thefirst temperature, the first temperature being greater than roomtemperature.
 8. The method of claim 7, wherein the cooling step includescooling the first solution to the second temperature, the secondtemperature being room temperature.
 9. The method of claim 1, whereinthe first solution is supersaturated with amorphous polycarbonate at thefirst temperature.
 10. The method of claim 1, wherein the partiallycrystalline polycarbonate powder has a D90 particle size of less thanabout 150 micrometers.
 11. The method of claim 1, wherein the partiallycrystalline polycarbonate powder has an average particle diameter fromabout 1 micrometer to about 100 micrometers.
 12. The method of claim 1,wherein the partially crystalline polycarbonate powder has an averageparticle diameter from about 30 micrometers to about 40 micrometers. 13.The method of claim 1, wherein the partially crystalline polycarbonatepowder is in the form of spheroidal particles.
 14. The method of claim1, wherein the partially crystalline polycarbonate powder has at leastabout 20% crystallinity.
 15. The method of claim 1, wherein thepartially crystalline polycarbonate powder has a crystallinity betweenabout 25% and about 35%.
 16. (canceled)
 17. (canceled)
 18. A method ofpreparing an object comprising: preparing a partially crystallinepolycarbonate powder according to the method of claim 1; and using thepartially crystalline polycarbonate powder in a powder bed fusionprocess to form the object.
 19. (canceled)
 20. (canceled)